P/N: 95136-03
Category: Controls & Cables
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 1 Available |
The 95136-03 is a control quadrant assembly for Piper PA-34-200T Seneca II aircraft. This mechanical component translates cockpit lever inputs into engine control cable motion, managing throttle and powerplant commands from the flight deck. The quadrant interfaces with push-pull cables using clevis terminals, converting pilot inputs into precise engine control responses.
Installation requires verification against the aircraft's Illustrated Parts Catalog and compliance with Piper maintenance procedures to ensure proper cable alignment and control travel.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The 95136-03 is a control quadrant assembly for Piper PA-34-200T Seneca II aircraft. This mechanical component translates cockpit lever inputs into engine control cable motion, managing throttle and powerplant commands from the flight deck.
The QUADRANT CONTROL may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: As Removed. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the QUADRANT CONTROL. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the 95136-03.